View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 52619U 26145.64608753 +.00000000 +00000-0 +80656-4 0 00002
2 52619 53.2128 283.6413 0001012 33.4621 326.6435 15.08835151 02
| Epoch (UTC): | 25 May 2026 15:30:21 |
| Eccentricity: | 0.0001012 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 283.6413° |
| argument of perigee: | 33.4621° |
| revolutions per day: | 15.08835151 |
| mean anomaly at epoch: | 326.6435° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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